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Статті в журналах з теми "Helicopter dynamic systems"
Khalesi, Mohammad Hossein, Hassan Salarieh, and Mahmoud Saadat Foumani. "System identification and robust attitude control of an unmanned helicopter using novel low-cost flight control system." Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 234, no. 5 (August 27, 2019): 634–45. http://dx.doi.org/10.1177/0959651819869718.
Повний текст джерелаFahimi, Farbod. "Full formation control for autonomous helicopter groups." Robotica 26, no. 2 (March 2008): 143–56. http://dx.doi.org/10.1017/s0263574707003670.
Повний текст джерелаAbu Zarim, Mohamad Abu Ubaidah Amir, and Marja Azlima Omar. "Dynamic Mechanics of Rigid Helicopter Systems During Ditching." Transactions on Maritime Science 10, no. 2 (October 21, 2021): 439–47. http://dx.doi.org/10.7225/toms.v10.n02.013.
Повний текст джерелаLiu, Jianbo, Rongqiang Guan, Yongming Yao, Hui Wang, and Linqiang Hu. "A Novel Comprehensive Kinematic and Inverse Dynamic Model for the Flybar-Less Swashplate Mechanism: Application on a Small-Scale Unmanned Helicopter." Symmetry 12, no. 11 (November 9, 2020): 1849. http://dx.doi.org/10.3390/sym12111849.
Повний текст джерелаGildish, Eli, Michael Grebshtein, Yehudit Aperstein, Alex Kushnirski, and Igor Makienko. "Helicopter Bolt Loosening Monitoring using Vibrations and Machine Learning." PHM Society European Conference 7, no. 1 (June 29, 2022): 146–55. http://dx.doi.org/10.36001/phme.2022.v7i1.3322.
Повний текст джерелаMa, Rui, Li Ding, and Hongtao Wu. "Dynamic Decoupling Control Optimization for a Small-Scale Unmanned Helicopter." Journal of Robotics 2018 (June 27, 2018): 1–12. http://dx.doi.org/10.1155/2018/9897684.
Повний текст джерелаWang, Jialiang, Hai Zhao, Yuanguo Bi, Shiliang Shao, Qian Liu, Xingchi Chen, Ruofan Zeng, Yu Wang, and Le Ha. "An Improved Fast Flocking Algorithm with Obstacle Avoidance for Multiagent Dynamic Systems." Journal of Applied Mathematics 2014 (2014): 1–13. http://dx.doi.org/10.1155/2014/659805.
Повний текст джерелаBittanti, Sergio, Fabrizio Lorito, and Silvia Strada. "An LQ Approach to Active Control of Vibrations in Helicopters." Journal of Dynamic Systems, Measurement, and Control 118, no. 3 (September 1, 1996): 482–88. http://dx.doi.org/10.1115/1.2801171.
Повний текст джерелаDe Pratti, Giovanni Maria. "Airfoil to Improve Aerodynamic Performance OF Aileron Reduced Spanwise in Combat Helicopter." E3S Web of Conferences 197 (2020): 11003. http://dx.doi.org/10.1051/e3sconf/202019711003.
Повний текст джерелаGuivarch, D., E. Mermoz, Y. Marino, and M. Sartor. "Creation of helicopter dynamic systems digital twin using multibody simulations." CIRP Annals 68, no. 1 (2019): 133–36. http://dx.doi.org/10.1016/j.cirp.2019.04.041.
Повний текст джерелаДисертації з теми "Helicopter dynamic systems"
Kontitsis, Michail. "Design and implementation of an integrated dynamic vision system for autonomous systems operating in uncertain domains." [Tampa, Fla] : University of South Florida, 2009. http://purl.fcla.edu/usf/dc/et/SFE0002852.
Повний текст джерелаSamal, Mahendra Engineering & Information Technology Australian Defence Force Academy UNSW. "Neural network based identification and control of an unmanned helicopter." Awarded by:University of New South Wales - Australian Defence Force Academy. Engineering & Information Technology, 2009. http://handle.unsw.edu.au/1959.4/43917.
Повний текст джерелаLopes, Darby Freitas de Albuquerque. "Estimativa da atitude e posição e controle robusto de um helicóptero autônomo." Universidade de São Paulo, 2010. http://www.teses.usp.br/teses/disponiveis/18/18153/tde-08022011-095400/.
Повний текст джерелаThis work concerns the study of an inertial reference system and a control system for an autonomous helicopter using, as basis for the formulation and testing, the linearized mo del of the aircraft Yamaha R-MAX. An inertial navigation system (INS) and an attitude and orientation reference system (AHRS) are used to estimate the position and attitude of the aircraft and robust estimators based on Kalman filter are employed to minimize the effects of parametric uncertainties. A cascaded control architecture with three control methodologies is used, consisting of an inner-loop to ensure stability of the helicopter (the LQR and H \'INFINITE\' techniques are used, separately), a mid-loop based on linearization feedback (FLC) to decouple the dynamics ofthe lateral, longitudinal, vertical and heading axes and an outer-loop based on a proportional-derivative (PD) controller to enable trajectory tracking. Simulation results are presented to evaluate the performance of each approach.
Guivarch, Damien. "Méthodes et outils d'aide à l'estimation des efforts sur les ensembles mécaniques en phase d'architecture. Application aux hélicoptères." Electronic Thesis or Diss., Toulouse, INSA, 2019. http://www.theses.fr/2019ISAT0053.
Повний текст джерелаNew software tools are used to simulate the transient dynamic behaviour of multi-body mechanical systems. Could they provide a good forecast of loads applied on helicopter rotary wing system? The work developed in this thesis provides some answers to this question, knowing that the context considered presents many difficulties: flexible bodies, complex mechanical links, hyperstatisms… The stakes are high because the development cycle of these mechanical assemblies would be greatly reduced by a correct estimation of loads during the first steps of the design of a new architecture. In this context, a new level of modeling is introduced, focusing on the dynamic systems studied. Since this level is part of a multi-scale approach, it is necessary to feed it with simplified models of the subassemblies that form the studied system, and this leads to so-called local studies. The presentation of this work is based on the rotary wing system of H160 helicopter, currently in industrialization phase at Airbus Helicopters, which includes the blades, the main rotor and the hydraulic control actuators. Three major developments are detailed: modelling of a swashplates sub-assembly, blades and the rotary wing system.The new modelling framework thus created allows the loads estimation at the level of the mechanical links of these systems and the monitoring of their evolution over time
Potter, James Jackson. "Input-shaped manual control of helicopters with suspended loads." Diss., Georgia Institute of Technology, 2013. http://hdl.handle.net/1853/50342.
Повний текст джерелаMittal, Manoj. "Modeling and control of a twin-lift helicopter system." Diss., Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/12174.
Повний текст джерелаBangalore, Ashok K. "Computational fluid dynamic studies of high lift rotor systems using distributed computing." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12949.
Повний текст джерелаNygren, Kip P. "An investigation of helicopter higher harmonic control using a dynamic system coupler simulation." Diss., Georgia Institute of Technology, 1986. http://hdl.handle.net/1853/12082.
Повний текст джерелаWeiner, Steven David 1956. "The effect of improved aircraft efficiency on helicopter sales using system dynamics." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/91712.
Повний текст джерелаBrown, Sean M. "Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/874.
Повний текст джерелаКниги з теми "Helicopter dynamic systems"
Jorgensen, Charles C. Analysis of tasks for dynamic man/machine load balancing in advanced helicopters. Oak Ridge, Tenn: Oak Ridge National Laboratory, 1987.
Знайти повний текст джерелаP, Townsend Dennis, Oswald Fred B, and United States. National Aeronautics and Space Administration., eds. Experimental and analytical evaluation of dynamic load and vibration of a 2240-kW (3000-hp) rotorcraft transmission. [Washington, DC: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаP, Townsend Dennis, Oswald Fred B, and United States. National Aeronautics and Space Administration., eds. Experimental and analytical evaluation of dynamic load and vibration of a 2240-kW (3000-hp) rotorcraft transmission. [Washington, DC: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Studies of the dynamics of the twin-lift system: Interim report. Princeton, NJ: Dept. of Mechanical and Aerospace Engineering, Princeton University, 1989.
Знайти повний текст джерелаL, Wilbur Matthew, U.S. Army Research Laboratory., and Langley Research Center, eds. Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаC, Curtiss H., and United States. National Aeronautics and Space Administration., eds. An analytic modeling and system identification study of rotor/fuselage dynamics at hover. [Washington, DC: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаK, Remple Robert, ed. Aircraft and rotorcraft system identification: Engineering methods with flight test examples. 2nd ed. Reston, VA: American Institute of Aeronautics and Astronautics, 2012.
Знайти повний текст джерелаK, Remple Robert, ed. Aircraft and rotorcraft system identification: Engineering methods with flight-test examples aircraft and rotorcraft system identification engineering methods with flight-test examples. Reston, VA: American Institute of Aeronautics and Astronautics, 2006.
Знайти повний текст джерелаV, Cook M., Rycroft Michael J, Institute of Mathematics and its Applications., and Conference on Aerospace Vehicle Dynamics and Control (1992 : Cranfield Institute of Technology), eds. Aerospace vehicle dynamics and control: Based on the proceedings of a conference organized by the Institute of Mathematics and its Applications on aerospace vehicle dynamics and control, held at the Cranfield Institute of Technology, in September 1992. Oxford: Clarendon Press, 1994.
Знайти повний текст джерелаBoden, Fritz. Advanced In-Flight Measurement Techniques. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.
Знайти повний текст джерелаЧастини книг з теми "Helicopter dynamic systems"
Zhang, Ke, Bin Jiang, and Peng Shi. "Helicopter Platform Applications." In Observer-Based Fault Estimation and Accomodation for Dynamic Systems, 157–66. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-33986-8_8.
Повний текст джерелаRen, Beibei, Shuzhi Sam Ge, Chang Chen, Cheng-Heng Fua, and Tong Heng Lee. "Dynamic Altitude Synchronization Using Graph Theory." In Modeling, Control and Coordination of Helicopter Systems, 195–216. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-1563-3_8.
Повний текст джерелаZhou, Jing, Lantao Xing, and Changyun Wen. "Adaptive Attitude Control of Helicopter with Quantization." In Adaptive Control of Dynamic Systems with Uncertainty and Quantization, 179–94. Boca Raton: CRC Press, 2021. http://dx.doi.org/10.1201/9781003176626-16.
Повний текст джерелаde Lope, Javier, Juan José San Martín, and José A. Martín H. "Helicopter Flight Dynamics Using Soft Computing Models." In Computer Aided Systems Theory – EUROCAST 2007, 621–28. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-75867-9_78.
Повний текст джерелаYue, Yi. "A System Dynamics Model for Helicopter Operations." In Operations Research/Management Science at Work, 405–21. Boston, MA: Springer US, 2002. http://dx.doi.org/10.1007/978-1-4615-0819-9_26.
Повний текст джерелаRen, Beibei, Shuzhi Sam Ge, Chang Chen, Cheng-Heng Fua, and Tong Heng Lee. "Altitude Control of Helicopters with Unknown Dynamics." In Modeling, Control and Coordination of Helicopter Systems, 59–92. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-1563-3_4.
Повний текст джерелаMasarati, Pierangelo, Andrea Zanoni, Vincenzo Muscarello, Rita Paolini, and Giuseppe Quaranta. "Helicopter Pilot Biomechanics by Multibody Analysis." In Nonlinear Dynamics of Structures, Systems and Devices, 439–47. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-34713-0_44.
Повний текст джерелаRen, Beibei, Shuzhi Sam Ge, Chang Chen, Cheng-Heng Fua, and Tong Heng Lee. "Attitude Control of Uncertain Helicopters with Actuator Dynamics." In Modeling, Control and Coordination of Helicopter Systems, 121–46. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-1563-3_6.
Повний текст джерелаRen, Beibei, Shuzhi Sam Ge, Chang Chen, Cheng-Heng Fua, and Tong Heng Lee. "Altitude and Yaw Control of Helicopters with Uncertain Dynamics." In Modeling, Control and Coordination of Helicopter Systems, 93–119. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-1563-3_5.
Повний текст джерелаZhang, Ruimin, Junbo Zhao, and Jingang Dong. "Simulation of Flight Dynamics for Helicopter Icing." In Proceedings of the 14th International Conference on Man-Machine-Environment System Engineering, 341–48. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-662-44067-4_41.
Повний текст джерелаТези доповідей конференцій з теми "Helicopter dynamic systems"
Kumar, Anil, and Pinhas Ben-Tzvi. "An Inertial Sensor to Measure Wind Turbulence With RC Helicopters." In ASME 2017 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/dscc2017-5354.
Повний текст джерелаPotter, James, Ryan Simpson, and William Singhose. "Dynamic Modeling and Simulation of a Remote-Controlled Helicopter With a Suspended Load." In ASME 2013 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/dscc2013-3998.
Повний текст джерелаTekes, Ayse, Adeel Khalid, Niko Giannakakos, and Alexander Bryant. "Helicopter Swashplate Design and Analysis Using Semi Compliant Mechanism." In ASME 2018 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/dscc2018-8944.
Повний текст джерелаKuntz, Noah R., and Paul Y. Oh. "Development of Autonomous Cargo Transport for an Unmanned Aerial Vehicle Using Visual Servoing." In ASME 2008 Dynamic Systems and Control Conference. ASMEDC, 2008. http://dx.doi.org/10.1115/dscc2008-2203.
Повний текст джерелаTaylor, James H., and Saied S. Sharif. "Chaos in nonlinear dynamic systems: Helicopter vibration mechanisms." In 2007 Mediterranean Conference on Control & Automation. IEEE, 2007. http://dx.doi.org/10.1109/med.2007.4433847.
Повний текст джерелаPounds, Paul E. I., and Aaron Dollar. "Hovering Stability of Helicopters With Elastic Constraints." In ASME 2010 Dynamic Systems and Control Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/dscc2010-4166.
Повний текст джерелаParsons, Matthew R., and Robert G. Langlois. "Stability Analysis of a Two-dimensional Tethered Helicopter." In International Conference of Control, Dynamic Systems, and Robotics. Avestia Publishing, 2016. http://dx.doi.org/10.11159/cdsr16.128.
Повний текст джерелаMolina, Javier, and Shinichi Hirai. "Dynamic landing gear for balancing a multirotor helicopter." In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2017. http://dx.doi.org/10.1109/icuas.2017.7991346.
Повний текст джерелаSeo, Joohwan, and Jongeun Choi. "Output Feedback Control Synthesis for a Helicopter Using Explicit Nonlinear Model Predictive Control, Dynamic Inversion and Extended High Gain Observers." In ASME 2019 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/dscc2019-9036.
Повний текст джерелаKumar, Anil, and Pinhas Ben-Tzvi. "Extraction of Impact of Wind Turbulence on RC Helicopters Using Machine Learning." In ASME 2016 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/detc2016-59384.
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